The invention discloses an anti-crosswind vertical take-off and landing unmanned aerial vehicle and an anti-crosswind method thereof, and relates to the technical field of unmanned aerial vehicles. The anti-crosswind vertical take-off and landing unmanned aerial vehicle comprises an unmanned aerial vehicle body and an anemorumbometer which is arranged in a manner of being separated from the unmanned aerial vehicle body; the unmanned aerial vehicle body comprises a fuselage, a flight control machine arranged in the fuselage, wings arranged on the two sides of the fuselage, propellers arranged in front of the wings, motors in transmission connection with the propellers, control surfaces arranged behind the wings and steering engines in transmission connection with the control surfaces, wherein the anemorumbometer is in communication connection with the flight control machine, and the flight control machine is connected with the motors and the steering engines through cables. Wind speed and wind direction information is measured through the anemorumbometer, steering engines are controlled to deflect and motors are controlled to rotate according to the wind speed and wind direction information, attitude information and height information, so that the orientation, height and yaw of the aircraft are controlled, the extension direction of wings and the crosswind direction are consistent, operation of a drone pilot is not needed, dependence on experience of the drone pilot is not needed, and the aircraft is prevented from landing under the condition that the attitude is inclined.

    本发明公开了一种抗侧风垂直起降无人机及其抗侧风方法,涉及无人机技术领域,抗侧风垂直起降无人机,包括无人机本体和与无人机本体分体设置的风速风向仪,无人机本体包括机身、设置于机身内的飞控机、设置于机身两侧的机翼、设置于机翼前方的螺旋桨、与螺旋桨传动连接的电机、设置于机翼后方的舵面、与舵面传动连接的舵机,风速风向仪与飞控机通讯连接,飞控机与电机、舵机线缆连接。通过风速风向仪测得风速风向信息,根据风速风向信息、姿态信息和高度信息,控制舵机偏转并控制电机转动,从而控制飞机朝向、高度和偏航,使机翼展长方向和侧风方向一致,不需要飞手操纵,更不需要依赖飞手经验,避免飞机在有姿态倾斜的情况下着陆。


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    Titel :

    Anti-crosswind vertical take-off and landing unmanned aerial vehicle and anti-crosswind method thereof


    Weitere Titelangaben:

    抗侧风垂直起降无人机及其抗侧风方法


    Beteiligte:
    SHAO PENGYUAN (Autor:in) / DONG YANFEI (Autor:in) / QU GAOMIN (Autor:in) / LI JIGUANG (Autor:in) / ZHU HANXIAO (Autor:in)

    Erscheinungsdatum :

    2021-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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